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A Review of the Proposed K (sub Isi) Offset-Secant Method for Size-Independent Linear-Elastic Toughness Evaluation The proposed size-independent linear-elastic fracture toughness, K (sub Isi), for potential inclusion in ASTM E399 targets a consistent 0.5 millimeters crack extension for all specimen sizes through an offset secant that is a function of the specimen ligament length. The K (sub Isi) method also includes an increase in allowable deformation, and the removal of the P (sub max)/P (sub Q) criterion. A finite element study of the K (sub Isi) test method confirms the viability of the increased deformation limit, but has also revealed a few areas of concern. Findings: 1. The deformation limit, b (sub o) greater than or equal to 1.1 times (K (sub I) divided by delta (sub ys) squared) maintains a K-dominant crack tip field with limited plastic contribution to the fracture energy; 2. The three dimensional effects on compliance and the shape of the force versus CMOD (Crack-Mouth Opening Displacement) trace are significant compared to a plane strain assumption; 3. The non-linearity in the force versus CMOD trace at deformations higher than the current limit of 2.5 times (K (sub I) divided by delta (sub ys) squared) is sufficient to introduce error or even "false calls" regarding crack extension when using a constant offset secant line. This issue is more significant for specimens with W (width) greater than or equal to 2 inches; 4. A non-linear plasticity correction factor in the offset secant may improve the viability of the method at deformations between 2.5 times (K (sub I) divided by delta (sub ys) squared) and 1.1 times (K (sub I) divided by delta (sub ys) squared).
Document ID
20170005327
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
James, Mark
(Arconic Technology Center New Kensington, PA, United States)
Wells, Doug
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Allen, Phillip
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wallin, Kim
(Technical Research Centre of Finland Espoo, Finland)
Date Acquired
June 7, 2017
Publication Date
May 10, 2017
Subject Category
Structural Mechanics
Report/Patent Number
M17-6005
Report Number: M17-6005
Meeting Information
Meeting: International ASTM/ESIS Symposium on Fatigue and Fracture Mechanics
Location: Toronto, ON
Country: Canada
Start Date: May 10, 2017
End Date: May 12, 2017
Sponsors: European Structural Integrity Society, ASTM International
Distribution Limits
Public
Copyright
Public Use Permitted.
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